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Calculation of supersonic steady-state flow in axisymmetric nozzles with an upwind difference scheme

✍ Scribed by Huang Lanjie

Book ID: 112761172
Publisher: The Chinese Society of Theoretical and Applied Mechanics; Institute of Mechanics, Chinese Academy of Sciences
Year: 1985
Tongue: English
Weight: 408 KB
Volume: 1
Category: Article
ISSN: 0567-7718
DOI: 10.1007/bf02487856

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